CN1333183C - Rotary damper device - Google Patents

Abstract

The invention relates to a damper device capable of keeping constant accuracy of braking torque, improving the durability by not applying heavy load to a valve and reducing the braking torque in non-braking. A first rotary blade 54 moved in silicone oil 41, extended in the radial direction to define an accommodating part 15 of a housing 11, 21 accommodating the silicone oil and having a notch 54a, is mounted on a rotor 51, a first valve 61 is mounted on the first rotary blade for opening the notch 54a in rotating the rotor in one direction and closing the notch 54a in rotating the rotor in the other direction, a second rotary blade 17 moved in the silicone oil, extended in the radial direction to define the accommodating part of the housing and having a notch 17a, is mounted on the housing, and a second valve 31 is mounted on the second rotary blade to open the notch 17a in rotating the rotor in one direction and closing the notch 17a in rotating the rotor in the other direction.

Description

Damper device

Technical field

The present invention relates to that subtend for example opens that the rotation of the door of direction is braked and unidirectional damper device that the rotation of the door of subtend closing direction is not braked.

Background technique

The scheme that above-mentioned damper device proposes in No. 2581655 communique of patent documentation 1-Japan Patent is by shell, be contained in the viscous fluid in this shell, rotatably be loaded in the shell, have, prevent that viscous fluid from constituting from the sealed member that leaks between the axial region of this rotor and the shell from the rotor of the outstanding a part of axial region of shell; The teat that will have the fluid passage on rotor is arranged on axially, covers the valve with the 1st fluid passage and the 2nd fluid passage on teat; Wherein, during the rotation of direction, viscous fluid is a small flow to the flow of the fluid passage of teat at rotor in the 1st fluid passage; During another direction rotation, viscous fluid is big flow to the flow of the fluid passage of teat at rotor in the 2nd fluid passage.

Because the valve of above-mentioned damper device can move, can dispose rotatably, thereby, by means of viscous fluid by and shell between the gap, can not obtain desired braking moment, be difficult to braking moment is kept certain precision.

And, because valve is imposed bigger load, thereby the danger of valve existence damage, its durability is also low.

Summary of the invention

The object of the present invention is to provide a kind of damper device, it can keep braking moment certain precision, can improve the durability of valve and valve is not applied big load, the braking moment when reducing non-braking simultaneously.

The present invention is following invention:

(1), damper device of the present invention, comprise following component: shell, be contained in the viscous fluid in the above-mentioned shell, rotatably be loaded on the rotor in the above-mentioned shell, and prevent the Sealing of above-mentioned viscous fluid from leaking between above-mentioned rotor and the above-mentioned shell; Wherein, the 1st rotation wing is arranged on a side of above-mentioned shell and above-mentioned rotor, and rotates the opposing party that the wing is arranged on above-mentioned shell and above-mentioned rotor the 2nd; The above-mentioned the 1st rotates that the wing has the 1st viscous fluid passage and to circumferencial direction relative movement and extend at radial direction and to make it separate the accommodating part of the above-mentioned shell that accommodates above-mentioned viscous fluid in above-mentioned viscous fluid; The above-mentioned the 2nd rotates that the wing has the 2nd viscous fluid passage and to circumferencial direction relative movement and extend at radial direction and to make it separate above-mentioned accommodating part in above-mentioned viscous fluid; Be provided with the 1st valve on above-mentioned the 1st rotation wing, above-mentioned the 1st valve is opened above-mentioned the 1st viscous fluid passage at above-mentioned rotor during a direction rotation, and closes above-mentioned the 1st viscous fluid passage at above-mentioned rotor during the other direction rotation; Be provided with the 2nd valve on above-mentioned the 2nd rotation wing, above-mentioned the 2nd valve is opened above-mentioned the 2nd viscous fluid passage at above-mentioned rotor during a direction rotation, and closes above-mentioned the 2nd viscous fluid passage at above-mentioned rotor during the other direction rotation.

(2), in the damper device of (1), wherein, on above-mentioned shell, be provided with towards the outstanding wall portion of the axial region direction of above-mentioned rotor, will have and the face of the above-mentioned wall portion of the orthogonal component face of the spin axis quadrature of above-mentioned rotor and and this face opposed, have and the face of the above-mentioned rotor of the orthogonal component face of above-mentioned spin axis quadrature between as the passage that compressed above-mentioned viscous fluid is passed through.

(3), in the damper device of (1) or (2), wherein, above-mentioned at least the 1st valve is formed by the elastomer of elastically deformable.

(4), in the damper device of (3), wherein, above-mentioned the 1st valve at least with the internal surface Elastic Contact of above-mentioned shell.

(5), in (1)-(4) in each the damper device, wherein, above-mentioned viscous fluid is a silicone oil, above-mentioned the 1st valve is made by the ethylene propylene diene rubber that above-mentioned silicone oil is had non-swelling.

Adopt the present invention, owing to will have the 1st viscous fluid passage and to circumferencial direction relative movement and extend at radial direction and to make it separate the 1st of the accommodating part that accommodates viscous fluid to rotate wing and be arranged between shell or the rotor in viscous fluid, during a direction rotation, open the 1st viscous fluid passage and on the 1st rotation wing, be provided with at rotor, and during other direction rotation, close the 1st valve of the 1st viscous fluid passage at rotor, thereby, when braking moment takes place, by means of close the 1st viscous fluid passage reliably with the 1st valve, then viscous fluid only by predetermined passage, can keep braking moment certain precision.

And, owing to will have the 2nd viscous fluid passage and to circumferencial direction relative movement and extend at radial direction and to make it separate the 2nd of the accommodating part that accommodates viscous fluid to rotate wing and be arranged between shell or the rotor in viscous fluid, during a direction rotation, open the 2nd viscous fluid passage and on the 2nd rotation wing, be provided with at rotor, and during other direction rotation, close the 2nd valve of the 2nd viscous fluid passage at rotor, thereby, by means of making compressed viscous fluid at least by the 1st viscous fluid passage and the 2nd viscous fluid passage, thereby make the viscous fluid in non-when braking that braking moment not take place, the braking moment in the time of can be with non-braking reduces very for a short time.

In addition, owing to, can reduce the load of the 1st valve, thereby can improve the durability of the 1st valve, and then also can improve the durability of damper device by establishing the 2nd valve.

Moreover, because the outstanding wall portion towards the axial region direction of rotor is set on shell, to have with the face of the wall portion of the orthogonal component face of the spin axis quadrature of rotor and opposed with this face, have face with the rotor of the orthogonal component face of spin axis as the passage that compressed viscous fluid is passed through, thereby, the interval of passage keeps certain because of the rigidity of shell, by this, can make braking moment keep certain precision.

And, owing to can make the member that forms passage have rigidity, thereby can improve the durability of damper device.

And then, owing to the elastomer of at least the 1 valve by elastically deformable forms, thereby the durability of the 1st valve can be improved, and then the durability of damper device can be improved.

In addition, owing to make the internal surface Elastic Contact of the 1st valve and shell at least, thereby can make viscous fluid reliably only by predetermined passage, can further improve the precision of braking moment.

Have, because viscous fluid is silicone oil, and the 1st valve uses the ethylene propylene diene rubber that silicone oil is had a non-swelling to make, thereby it is bad that valve can not occur moving to temperature variation, even also can normally use at cold zone again.

Description of drawings

Fig. 1 is the exploded perspective view of the damper device of one embodiment of the present of invention.

Fig. 2 is the plan view of housing shown in Figure 1.

Fig. 3 is the front view of housing shown in Figure 2.

Fig. 4 is the worm's eye view of housing shown in Figure 2.

Fig. 5 is the sectional drawing along the A-A line of Fig. 2.

Fig. 6 is the sectional drawing along the B-B line of Fig. 2.

Fig. 7 is the plan view of lid shown in Figure 1.

Fig. 8 is the sectional drawing along the C-C line of Fig. 7.

Fig. 9 is the plan view of the 2nd valve shown in Figure 1.

Figure 10 is the front view of the 2nd valve shown in Figure 9.

Figure 11 is the worm's eye view of the 2nd valve shown in Figure 9.

Figure 12 is the plan view of rotor shown in Figure 1.

Figure 13 is the front view that the left side of rotor shown in Figure 12 is partly cutd open.

Figure 14 is the worm's eye view of rotor shown in Figure 12.

Figure 15 is the plan view of the 1st valve shown in Figure 1.

Figure 16 is the front view of the 1st valve shown in Figure 15.

Figure 17 is the worm's eye view of the 1st valve shown in Figure 15.

Figure 18 is the right side view of the 1st valve shown in Figure 15.

Figure 19 is the plan view of arm shown in Figure 1.

Figure 20 is the front view of the band partial cutaway of arm shown in Figure 19.

Figure 21 is the amplification profile along the D-D line of Figure 19.

Figure 22 is the plan view of the damper device of one embodiment of the present of invention.

Figure 23 is the front view of the damper device of one embodiment of the present of invention.

Figure 24 is the rear view of the damper device of one embodiment of the present of invention.

Figure 25 is the worm's eye view of the damper device of one embodiment of the present of invention.

Figure 26 is the right side view of the damper device of one embodiment of the present of invention.

Figure 27 is the left side view of the damper device of one embodiment of the present of invention.

Figure 28 is the partial sectional view along the E-E line of Figure 22.

Figure 29 is the amplification profile along the E-E line of Figure 22.

Figure 30 is the half sectional view along the amplification of the F-F line of Figure 22.

Figure 31 is the action specification figure of the damper device of one embodiment of the present of invention.

Figure 32 is the action specification figure of the damper device of one embodiment of the present of invention.

Figure 33 is the action specification figure of the damper device of one embodiment of the present of invention.

Figure 34 is the action specification figure of the damper device of one embodiment of the present of invention.

Embodiment

Below, embodiments of the invention are described with reference to the accompanying drawings.

Fig. 1 is the exploded perspective view of the damper device of one embodiment of the present of invention.

Among Fig. 1, D represents damper device, is made of following component: by the housing 11 made of polycarbonate (PC) for example of the synthetic resin with rigidity; Be used to seal the open part of this housing 11, by the lid 21 made of polycarbonate (PC) for example of the synthetic resin with rigidity; Be installed in the 2nd of the bottom that is arranged in the housing 11 rotate on the wing, by synthetic resin the 2nd valve 31 made of polyoxymethylene for example; As the silicone oil 41 that is contained in the viscous fluid of (accommodating part 15) in the housing 11 that covers 21 sealings; Rotatably be loaded in the shell 11, have from cover 21 through hole 22 to the outstanding a part of axial region 52 in outside, by the synthetic resin rotor 51 made of polyoxymethylene for example; Be installed in be arranged at the 1st on this rotor 51 rotate on the wing 54, by to viscous liquid for example silicone oil 41 have the 1st valve 61 that non-swelling and rubber-like ethylene propylene diene rubber are made; Prevent silicone oil 41 from cover 21 and rotor 51 between the Sealing, the O type circle 71 that forms by the silicone rubber of for example selflubricating that leak; External diameter is slightly littler than the external diameter of the lip part 53 of rotor 51, be configured in cover 21 and the lip part 53 of rotor 51 between the circular closure plate 81 made of synthetic resin; Be installed in from the axial region 52 that covers 21 outstanding rotors 51 by the arm 91 made of polyoxymethylene for example of the synthetic resin with rigidity.

In addition, shell is made of housing 11 and lid 21.

Fig. 2 is the plan view of housing shown in Figure 1, and Fig. 3 is the front view of housing shown in Figure 2, and Fig. 4 is the worm's eye view of housing shown in Figure 2, and Fig. 5 is the sectional drawing along the A-A line of Fig. 2, and Fig. 6 is the sectional drawing along the B-B line of Fig. 2.

In these figure, housing 11 is by constituting with the bottom: being provided with around plane shape is the enclosure body 12 of the cylindrical wall portion 14 that forms of bottom 13 outer rims of circle; The columned axle support 16 that 13 bottom center is provided with in the bottom; At the axle support 16 with the bottom surface of bottom 13 is on the symmetrical position at center, extends to axially (axial region 52 of rotor 51 axially) of axle support 16, extends to 2 the 2nd of cylindrical wall portion 14 to radial direction simultaneously and rotate the wings 17 apart from axle support 16 certain distances; And in the periphery of enclosure body 12 to the arm 18 that radially is provided with.

Interior all upsides in above-mentioned cylindrical wall portion 14 are provided with: the stepped part 14a that the downside diameter increases, the upper end of the stepped part 14a that increases from this downside diameter is the conus portion 14b that increases gradually of diameter upward, the stepped part 14c of the upside diameter that is connected with the upper end of this conus portion 14b increase.

The 2nd above-mentioned rotation wing 17 is towards the direction and the outstanding wall portion of double as of the axial region 52 of rotor 51; The 2nd rotates the axle supporting breach 17b that the wing 17 is provided with the breach 17a of the 2nd viscous fluid passage that circulates as silicone oil 41 and the 2nd valve 31 is installed; The 2nd valve 31 is used for rotor 51 at the 17a that makes a breach during a direction (clockwise direction of Fig. 2) rotation, and at rotor 51 sealing breach 17a during other direction (counter clockwise direction among Fig. 2) rotation.

And the 2nd height that rotates the wing 17 is taken as the level height with the lower surface sliding contact of the lip part 53 of rotor 51, and in addition, the 2nd interior all sides upper end of rotating the wing 17 makes the conical surface 17c that descends towards the center.

Front end at above-mentioned arm 18 is provided with mounting hole 18a.

In addition, 15 are illustrated in the accommodating part that forms in the enclosure body 12 (shell), are the parts of holding silicone oil 41, are equivalent to by housing 11 and lid 21 spaces that form.

And the accommodating part 15 that accommodates rotor 51 states is in the enclosure separated by the 1st rotation wing 54 of rotor 51 and the 2nd rotation wing 17.

Fig. 7 is the plan view of lid shown in Figure 1, and Fig. 8 is the sectional drawing along the C-C line of Fig. 7.

Among Fig. 7 or Fig. 8, be provided with the through hole 22 that the axial region 52 of rotor 51 passes at lid 21 center, be provided with stepped part 23 that lightening hole cylindraceous increases with the diameter that is used to hold O type circle so that O type circle can arrive the lower end at the downside of this through hole 22; And then, be provided with the upside diameter increase stepped part 25 that the conus portion 24 that increases gradually with the diameter upward of the conus portion 14b butt joint of enclosure body 12 and upper end with this conus portion 24 link to each other, dock with the upside diameter increase stepped part 14c of enclosure body 12 in lid 21 outer rim.

Fig. 9 is the plan view of the 2nd valve shown in Figure 1, and Figure 10 is the 2nd a valve front view shown in Figure 9, and Figure 11 is the worm's eye view of the 2nd valve shown in Figure 9.

In these figure, the 2nd valve 31 constitutes by the axial region 32 in the rotatable axle supporting breach 17b that inserts housing 11 rotatably with from the valve portion 33 that this axial region 32 extends, is used to open and close the breach 17a of housing 11.

In addition, though be provided with breach 33a at the downside of valve portion 33, the size of this breach 33a is made and do not form opening when being overlapped with the breach 17a of housing 11.

Figure 12 is the plan view of rotor shown in Figure 1, and Figure 13 is the front view that the left side of rotor shown in Figure 12 is partly cutd open, and Figure 14 is the worm's eye view of rotor shown in Figure 12.

In these figure, rotor 51 is by constituting with the bottom: columned axial region 52, be formed at the periphery of this axial region 52, be that the lip part 53 into circle is overlooked at the center with axial region 52, with lower surface at this lip part 53 with axial region 52 be on the symmetrical position at center from the periphery of axial region 52 radially (to radial direction) be connected be provided with and make that the accommodating part 15 of housing 11 separates the 1st rotate the wing 54.

On above-mentioned axial region 52, establish the columnar recess 52a that rotatably cooperates with the axle support 16 of housing 11 at underside side, establishing by the I-shaped cutting stepped part 52b of I-shaped cutting, the mating groove 52c of substantially horizontal is set respectively on the planar section (vertical surface) of I-shaped cutting from covering 21 through hole, 22 outstanding parts.

On above-mentioned lip part 53, be on the concentric circle at center with axial region 52, for example the interval with 180 degree is provided with 2 hole 53a.

The purpose that this lip part 53 is provided with is when moment described later is produced, and compartment (A) is unlikely to be directly passed to O type circle 71 because of the pressure that compression produces; This flange 53 make discoid so as to block the compartment (A) at silicone oil 41 places and compartment (B) and O type circle 71 between and O-ring barrel portion 14.

And, because when producing direction (clockwise direction among Figure 30) rotation to moment, compartment (A) produces malleation because of big compressive force, in case for silicone oil 41 enter cover 21 and lip part 53 between the time be formed for passage that silicone oil 41 is emitted, on the lip part 53 of rotor 51, be provided with hole 53a, so that make silicone oil 41 when producing the direction rotation, be positioned at the compartment (B) of the compartment that becomes negative pressure to moment, thereby, enter cover 21 and lip part 53 between silicone oil 41 flow to the compartment (B) of negative pressure by hole 53a, then can avoid taking place with silicone oil 41 be enclosed in cover 21 and lip part 53 between state and make faults such as covering 21 distortion.

In addition, owing to O type circle 71 is not applied load, thereby silicone oil 41 can not leak between rotor 51 and shell, can improve durability.

Rotate on the wing 54 the above-mentioned the 1st, be provided with as the breach 54a of the 1st viscous fluid passage of silicone oil 41 circulations and the axle supporting breach 54b of the 1st valve 61 is installed; The 1st valve is at rotor 51 54a that makes a breach during a direction (among Figure 12 for clockwise direction) rotation, and closes breach 54a at rotor 51 during other direction (among Figure 12 for counterclockwise) rotation.

In addition, the downside of the anastomosis part of axial region 52 and lip part 53, promptly make the conical surface 55 that narrows down gradually to downside with the opposed part of conical surface 17c of housing 11, between the conical surface 17c of this conical surface 55 and housing 11 as the passage 58 that the silicone oil 41 that is compressed (pressurization) is passed through.

Figure 15 is the plan view of the 1st valve shown in Figure 1, and Figure 16 is the front view of the 1st valve shown in Figure 15, and Figure 17 is the worm's eye view of the 1st valve shown in Figure 15, and Figure 18 is the right side view of the 1st valve shown in Figure 15.

In these figure, the 1st valve 61 is by constituting with the bottom: the interior axial region 62 of axle supporting breach 54b that is pressed into rotor 51, from this axial region 62 extend, the valve portion 63 of the breach 54a of switch rotor 51, up and down direction extend and is connected with the front end of this valve portion 63 be provided with, bear the pressure of the silicone oil 41 that is compressed (pressurization) and be used for prominent bar 64 effectively at the 63 obstruction breach 54a of valve portion.

Figure 19 is the plan view of arm shown in Figure 1, and Figure 20 is the front view of the partial cutaway of arm shown in Figure 19, and Figure 21 is the amplification profile along the D-D line of Figure 19.

In these figure, arm 91 is made of the 2nd horizontal part 94 that the 1st horizontal part 92, the rake 93 that links to each other with the right-hand member of this horizontal part 92 link to each other with right-hand member with this rake 93, and each several part 92-94 overlooks to being linked to be straight line shape.

On above-mentioned the 1st horizontal part 92, be provided with in the circular-arc center of left end and be cut into I-shaped mounting hole 92a, partly be respectively equipped with the prominent bar 92b of the cooperation that cooperates with the mating groove 52c of the axial region 52 that is arranged on rotor 51 at the vertical surface of this mounting hole 92a, make and cooperate prominent bar 92 can front and back mobile a little thereby be respectively equipped with weight reduction groove 92c in the outside of the prominent bar 92 of this cooperations.

On above-mentioned horizontal part 94,, be provided with circular mounting hole 94a in the circular-arc center of right-hand member.

Below, the example that damper device D assembles is described.

At first, the axial region 32 with the 2nd valve 31 rotatably inserts respectively in 2 axle supporting breach 17b of housing 11.

Then, the axial region 32 with the 1st valve 61 is pressed into respectively in 2 axle supporting breach 54b of rotor 51.

Secondly, an amount of silicone oil 41 is injected in the accommodating part 15, behind the downside of the recess 52b that applies rotor 51 with silicone oil, axial region 52 and lip part 53 etc., a part and the lip part 53 of axial region 52 is placed in the accommodating part 15, thereby makes the axle support 16 of housing 11 be coupled to recess 52a.

Like this, when in the accommodating part 15 of injecting silicone oil 41 that the part of axial region 52 and lip part 53 are packed into, owing on lip part 53, be provided with hole 53a, thereby the air of lip part 53 downsides (accommodating part 15 in) be when can discharge upward from hole 53a, and silicone oil 41 also overflows to the upside of lip part 53 a little from hole 53a.

Therefore, air can not infiltrated the downside (accommodating part 15 in) of lip part 53, can reduce to come from the fluctuation of the braking moment due to the air of having infiltrated in the accommodating part 15.

Then, tumble in O type circle 71 at axial region 52 with rotor 51, and after the outer rim of lip part 53 is put circular closure plate 81, the axial region 52 of rotor 51 inserted cover in 21 the through hole 22, and on one side O type circle is pressed into diameter and increases in the stepped part 23, make on one side and cover 21 conus portion 24 and dock with the conus portion 14b of housing 11, make the upside diameter increase stepped part 25 simultaneously and increase stepped part 14c with the upside diameter and dock, thereby with the opening portion that covers 21 enclosing housings 11.

Like this, when when covering the opening portion of 21 enclosing housings 11, the air of lip part 53 upsides nearly all is discharged to outside the shell, lip part 53 contact with circular closure plate 81 by silicone oil 41 with lid 21, diameter increase stepped part 23 interior O type circles 71 can prevent silicone oil 41 from cover 21 and axial region 52 between leakage.

Then, the upper end of housing 11 is inboard and cover between 21 the outer rim and make whole periphery welding and sealing with for example high frequency welding.

Then, when in the mounting hole 92a that will be pressed into arm 91,, can assemble, thereby finish the assembling of damper device D by the cooperation that cooperates raised line 92b and mating groove 52c as Figure 22-shown in Figure 30 from the axial region 52 that covers 21 outstanding rotors 51.

When such assembling damper device D, the 1st valve 61 becomes with the internal surface of shell, is the bottom surface and the inner peripheral surface of housing 11 and the state that covers 21 lower surface Elastic Contact, and reliably accommodating part 15 separated.

Figure 31-Figure 34 is the action specification figure of the damper device of explanation one embodiment of the present of invention.

Below its action is described.

The installation of damper device D is, for example housing 11 is installed at above-below direction on the opening portion of body of machine with arm 18, and arm 91 is installed in the 2nd horizontal part 94 on the lid of opening portion of Switch main body.

And the lid closing state is equivalent to Figure 31, and the state that lid is opened is equivalent to Figure 34.

At first, close at lid shown in Figure 31 under the state of opening portion of body, shown in the arrow among Figure 22, when being used to remove the arm 91 that omitted illustrated locking mechanism etc. and opened lid when counter clockwise direction is rotated, by rotor 51 rotation in the counterclockwise direction that is connected with lid through arm 91, because the silicone oil 41 of the A of compartment in the accommodating part 15 that is clipped in the middle by the 1st valve 61 and the 2nd valve 31 is compressed, shown in figure 32, the 1st valve 61 cuts out by means of the pressure of the silicone oil in the A of compartment 41 and is arranged on the breach 54a that the 1st on the rotor 51 rotates the wing 54, and the 2nd valve 31 cuts out the breach 17a that is arranged on the rotation of the 2nd on the housing 11 wing 17 by means of the pressure of the silicone oil in the A of compartment 41.

Therefore, breach 54a, 17a by the A of compartment of the 1st valve 61 and the sealing of the 2nd valve 31 in compressed silicone oil 41 be difficult to from the A of this compartment, extract out, thereby lid is braked in the rotational action of opening direction.

In addition, in the A of compartment compressed silicone oil 41 shown in the enlarged view of Figure 30, the adjacent B of compartment in passage 58 flows out to accommodating part 15.

Like this, when compressed silicone oil 41 passes through passage 58, has orthogonal component face with the spin axis quadrature of rotor 51 owing to form conical surface 55 that the 2nd of path 58 rotates the conical surface 17c of the wing 17 and rotor 51, promptly, because conical surface 17c, 55 can be decomposed into the normal surface and the parallel surface parallel with the spin axis of rotor 51 with the spin axis quadrature of rotor, and conical surface 17c, 55 have the normal surface (orthogonal component face) with the spin axis quadrature of rotor 51, thereby can make the bottom of housing 11 and rotor 51 be subjected to stress by the formed departure direction of pressure of the silicone oil 41 by passage 58, open thereby passage 58 is expanded, the interval of passage 58 keeps certain because of the rigidity of shell.Therefore, because the interval of passage 58 keeps certain, can make braking moment keep certain precision.

Then, rotate to open position and when having omitted illustrated brake component and contact, damper device D stops at state shown in Figure 33 when lid.

When under this state, lid being rotated for the opening portion of closing body, make arm 91 when the clockwise direction opposite with the direction of arrow shown in Figure 22 rotates, the silicone oil 41 because silicone oil 41 in the A of compartment is not compressed in the B of compartment is compressed, as shown in figure 34, the 1st valve 61 is owing to the pressure of the silicone oil 41 in the compressed B of compartment is opened the 1st breach 54a that rotates the wing 54, and the 2nd valve 31 is because the pressure of the silicone oil 41 in the compressed B of compartment is opened the breach 17a of the 2nd rotation wing 17.

Therefore, silicone oil 41 promptly moves (flowing) to the A of compartment from the B of compartment by following each several part, thereby makes lid become non-braking to the spinning movement of closing direction; These parts are: the 1st rotate in the breach 54a of the wing 54, the 1st rotate between the wing 54 and the cylindrical wall portion 14, the 2nd rotate in the breach 17a of the wing 17 and in the breach 33a of valve portion 33.

As mentioned above, adopt this embodiment of the present invention, rotate the wing 54 owing on rotor 51, be provided with the 1st, the 1st rotates the wing 54 has breach 54a, in silicone oil 41, move, make its accommodating part that separates the shell that holds silicone oil 41 15 to the radial direction extension to circumferencial direction, and on the 1st rotation wing 54, be provided with the 1st valve 61, the 1st valve is made with the elastomer of elastically deformable, at rotor 51 54a that during the rotation of direction, makes a breach, and during the other direction rotation, close breach 54a at rotor 51; Thereby, when braking moment takes place,, then can make 41 passages 58 of silicone oil, thereby braking moment can be kept certain precision by being scheduled to by sealing breach 54a reliably with the 1st valve 61.

Moreover, owing on the 2nd rotation wing 17, be provided with the 2nd valve 31, above-mentioned the 2nd valve 31 is at rotor 51 17a that makes a breach during the rotation of direction, and during the other direction rotation, close breach 17a at rotor 51, thereby, for braking moment is not occurred in the silicone oil 41 in non-when braking, by making compressed silicone oil 41 at least by 2 breach 17a, 54a, the braking moment in the time of then can reducing non-braking.

In addition, because by establishing the load that the 2nd valve 31 can alleviate the 1st valve 61, thereby can improve the durability of the 1st valve, thus the durability of damper device D also improved.

And then, owing on shell, be provided with towards the outstanding wall portion of axial region 52 directions of rotor 51 (the 2nd rotates the wing 17), will have and the face (17c) of the wall portion of the orthogonal component face of the spin axis quadrature of rotor 51 and and this face (17c) opposed, have and the face 55 of the rotor 51 of the orthogonal component face of the spin axis quadrature of rotor 51 between as the passage 58 that compressed silicone oil 41 is passed through; Thereby because when braking moment takes place, passage 58 expands out because of the pressure of the silicone oil 41 by passage 58, and the interval of passage 58 keeps necessarily because of the rigidity of shell, thereby can make braking moment keep certain precision.

And, owing to can make the shell and the rotor 51 that form passage 58 have rigidity, thereby can improve the durability of damper device D.

Have again, owing to the 1st valve 61 is made with the elastomer of elastically deformable, thereby can improve the durability of the 1st valve 61, thereby also can improve the durability of damper device D.

And, owing to make the 1st valve 61 and the internal surface of shell and the outer surface Elastic Contact of rotor, thereby, can make silicone oil 41 reliably only by predetermined passage 58, can further improve the precision of braking moment.

And then, because the 1st valve 61 makes with the ethylene propylene diene rubber that silicone oil 41 is had non-swelling, thus 61 pairs of temperature variation of the 1st valve can not occur moving bad, even also can normally use at cold zone.

And, since between the lid 21 and the lip part 53 of rotor 51 annular enclosed 81 of layout circle, thereby, when beginning to move, silicone oil 41 can not diffuse in cover 21 and rotor 51 between, can reduce cover 21 and rotor 51 between the surface friction drag that taken place.

In the above-described embodiment, though expression is the example that the 2nd valve 31 is made with synthetic resin, the 2nd valve also can be made with elastomer.

And, though the example of representing as viscous fluid that is to use silicone oil 41 also can use other viscous fluid with said function, for example lubricating grease etc.

In addition, though expression is to establish the 2nd to rotate the wing 17 on shell, when on the 2nd rotation wing 17, establishing the 2nd valve 31, on rotor 51, establish the 1st and rotate the wing 54, rotate the example of establishing the 1st valve 61 on the wing 54 the 1st, even but adopt and on shell, establish the 1st rotation wing, when on the 1st rotation wing, establishing the 1st valve, on rotor, establish the 2nd and rotate the wing, rotate the structure of establishing the 2nd valve on the wing, also can obtain same effect the 2nd.

Like this, rotate the wing owing on shell, establish the 1st, when on the 1st rotation wing, establishing the 1st valve, on rotor, establish the 2nd and rotate the wing, rotate on the wing the 2nd and establish under the situation of the 2nd valve, because 2 valves all adopt the structure that is pressed into installation, each valve all can not rotate the wing from it, thereby assembling operation carries out easily, can carry out the assembling of damper device D expeditiously.

In addition, though expression is with breach 17a, the 54a example as each viscous fluid passage, by with the hole as each viscous fluid passage, also can open and close each viscous fluid passage reliably.

Have again, though expression is to make the axial region of rotor 51 protrude in the example of shell, but also can adopt following structure: do not make the axial region of rotor protrude in shell, but cooperating recesses is set at the axial region of the rotor that exposes from shell, connected element is cooperated with this cooperating recesses and the rotor opposite shell is rotated.

And,, obviously, also can be only form with normal surface with the spin axis quadrature of rotor 51 though expression is the example that forms passages 58 with conical surface 17C, 55.

In addition, though expression is the example that forms the 2nd valve 61 with inelastic body, also can obtain same effect even form the 2nd valve with elastomer.

Moreover, though expression is the example that forms O type circle with the silicone rubber of selflubricating, but O type circle is by making with the ethylene propylene diene rubber that silicone oil 41 is had non-swelling, then can reduce of the change of O type circle, thereby even also can normally use at cold zone because of the braking moment due to being acted upon by temperature changes.

In addition, though expression is to have following example of structure, that is: shell is made of housing 11 and lid 21, is provided with the accommodating part 15 of silicone oil 41 on housing 11, on lid 21, be provided with the through hole 22 that the axial region 52 of rotor 51 passes, with O type circle 71 prevent silicone oil 41 from cover 21 and axial region 52 between leak; But also can adopt following structure, that is: cover the accommodating part that silicone oil is set, the through hole that the axial region of rotor passes is set on housing, and prevent that with O type circle silicone oil from leaking between housing and axial region.

Claims (7)

1. damper device comprises following component:

Shell,

Be contained in the viscous fluid in the above-mentioned shell,

Rotatably be loaded on the rotor in the above-mentioned shell, and

Prevent the Sealing of above-mentioned viscous fluid from leaking between above-mentioned rotor and the above-mentioned shell;

It is characterized in that:

The 1st rotation wing is arranged on a side of above-mentioned shell and above-mentioned rotor, and rotates the opposing party that the wing is arranged on above-mentioned shell and above-mentioned rotor the 2nd;

The above-mentioned the 1st rotates that the wing has the 1st viscous fluid passage and to circumferencial direction relative movement and extend at radial direction and to make it separate the accommodating part of the above-mentioned shell that accommodates above-mentioned viscous fluid in above-mentioned viscous fluid;

The above-mentioned the 2nd rotates that the wing has the 2nd viscous fluid passage and to circumferencial direction relative movement and extend at radial direction and to make it separate above-mentioned accommodating part in above-mentioned viscous fluid;

Be provided with the 1st valve on above-mentioned the 1st rotation wing, above-mentioned the 1st valve is opened above-mentioned the 1st viscous fluid passage at above-mentioned rotor during a direction rotation, and closes above-mentioned the 1st viscous fluid passage at above-mentioned rotor during the other direction rotation;

Be provided with the 2nd valve on above-mentioned the 2nd rotation wing, above-mentioned the 2nd valve is opened above-mentioned the 2nd viscous fluid passage at above-mentioned rotor during a direction rotation, and closes above-mentioned the 2nd viscous fluid passage at above-mentioned rotor during the other direction rotation.

2. damper device according to claim 1 is characterized in that:

On above-mentioned shell, be provided with towards the outstanding wall portion of the axial region direction of above-mentioned rotor,

To have and the face of the above-mentioned wall portion of the orthogonal component face of the spin axis quadrature of above-mentioned rotor and and this face opposed, have and the face of the above-mentioned rotor of the orthogonal component face of above-mentioned spin axis quadrature between as the passage that compressed above-mentioned viscous fluid is passed through.

3. damper device according to claim 1 and 2 is characterized in that:

At least above-mentioned the 1st valve is formed by the elastomer of elastically deformable.

4. damper device according to claim 3 is characterized in that:

Above-mentioned the 1st valve at least with the internal surface Elastic Contact of above-mentioned shell.

5. according to each described damper device among the claim 1-2, it is characterized in that:

Above-mentioned viscous fluid is a silicone oil,

Above-mentioned the 1st valve is made by the ethylene propylene diene rubber that above-mentioned silicone oil is had non-swelling.

6. according to the damper device described in the claim 3, it is characterized in that:

Above-mentioned viscous fluid is a silicone oil,

Above-mentioned the 1st valve is made by the ethylene propylene diene rubber that above-mentioned silicone oil is had non-swelling.

7. according to the damper device described in the claim 4, it is characterized in that:

Above-mentioned viscous fluid is a silicone oil,

Above-mentioned the 1st valve is made by the ethylene propylene diene rubber that above-mentioned silicone oil is had non-swelling.

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